BE Computer Engineering (IOE, TU) Numerical Methods (IOE, SH 553) Question Paper 2079 Nepal
This is the official BE Computer Engineering (IOE, TU) Numerical Methods (IOE, SH 553) question paper for 2079, as set in the regular annual examination. It carries 80 full marks and a time allowance of 180 minutes, across 11 questions. On Kekkei you can attempt this Numerical Methods (IOE, SH 553) past paper online with a timer, get instant AI feedback and step-by-step solutions, and track the topics where you lose marks — completely free. Whether you are revising for your BE Computer Engineering (IOE, TU) Numerical Methods (IOE, SH 553) exam or solving previous years' question papers, this 2079 paper is a great way to practise under real exam conditions.
Section A: Long Answer Questions
Attempt all / any as specified.
(a) Derive the iterative formula for the Newton-Raphson method for finding a root of a nonlinear equation , and state its order of convergence. Discuss two situations in which the method fails. [7]
(b) Using the Bisection method, find a root of the equation correct to three decimal places. Show the tabulation of iterations. [5]
(a) Newton-Raphson Method
Derivation. Let be an approximation to a root of and let be the correction so that . Expanding by Taylor's series and retaining only first-order terms:
Hence the iterative formula is
Order of convergence. Writing the error about the simple root gives
Thus the method converges quadratically (order ) for a simple root.
Two situations in which the method fails:
- (near a turning point / stationary point): the correction becomes very large and the iterate is thrown far away, so the method diverges.
- Poor initial guess / oscillation: if is not close enough to the root, or where the curve has a near-horizontal tangent or an inflection, the iterates may oscillate between two values or diverge. (It also fails / loses its quadratic rate at a multiple root, where .)
(b) Bisection Method for
Let . Since and , a root lies in .
| n | a | b | c=(a+b)/2 | f(c) | sign |
|---|---|---|---|---|---|
| 1 | 2.000 | 3.000 | 2.5000 | ||
| 2 | 2.500 | 3.000 | 2.7500 | ||
| 3 | 2.500 | 2.750 | 2.6250 | ||
| 4 | 2.625 | 2.750 | 2.6875 | ||
| 5 | 2.6875 | 2.750 | 2.7188 | ||
| 6 | 2.6875 | 2.7188 | 2.7031 | ||
| 7 | 2.7031 | 2.7188 | 2.7109 | ||
| 8 | 2.7031 | 2.7109 | 2.7070 | ||
| 9 | 2.7031 | 2.7070 | 2.7051 | ||
| 10 | 2.7051 | 2.7070 | 2.7061 | ||
| 11 | 2.7061 | 2.7070 | 2.7065 |
Continuing until the interval , the iterates settle at
correct to three decimal places.
(a) Derive Newton's divided difference interpolation formula and show that the divided differences are symmetric with respect to their arguments. [6]
(b) The following table gives the values of a function :
| x | 5 | 6 | 9 | 11 |
|---|---|---|---|---|
| f(x) | 12 | 13 | 14 | 16 |
Using Lagrange's interpolation formula, estimate the value of at . [6]
(a) Newton's Divided Difference Formula
For data the divided differences are defined recursively by
Interpolating polynomial. Assume
Putting gives ; putting gives ; in general . Hence Newton's divided difference formula:
Symmetry. By induction it can be shown that
This expression is a symmetric function of — interchanging any two arguments leaves it unchanged. Therefore the divided differences are symmetric with respect to their arguments, i.e.
(b) Lagrange Interpolation at
Data: . Lagrange's formula:
At :
(a) Explain the Gauss-Seidel iterative method for solving a system of linear equations. State the condition of convergence (diagonal dominance) for the method. [5]
(b) Solve the following system of equations using the Gauss-Seidel iteration method, performing three iterations and starting with the initial approximation :
[7]
(a) Gauss-Seidel Iterative Method
For a system , each equation is solved for its diagonal unknown:
The distinguishing feature is that each newly computed value is used immediately in the same sweep, so it generally converges faster than Jacobi iteration. Iteration continues until successive iterates agree to the required tolerance.
Condition of convergence (diagonal dominance). A sufficient condition is that the coefficient matrix be diagonally dominant:
Under this condition the iteration converges for any starting vector.
(b) Three Iterations, start
The system is already diagonally dominant. Rearranging:
Iteration 1 (with initially):
Iteration 2:
Iteration 3:
| Iter | x | y | z |
|---|---|---|---|
| 1 | 0.8500 | 1.0109 | |
| 2 | 1.0025 | 0.9998 | |
| 3 | 1.0000 | 1.0000 |
(a) Derive the standard five-point finite-difference formula for the Laplace equation over a square mesh. [6]
(b) Classify the partial differential equation as elliptic, parabolic or hyperbolic, and give one physical example of each type. [6]
(a) Five-Point Formula for the Laplace Equation
Use a uniform square mesh of spacing (); let . Central second differences give
Substituting into and multiplying by :
This standard five-point (cross) formula states that the value at any interior node equals the average of its four nearest neighbours (Liebmann's method solves the resulting set iteratively).
(b) Classification of
The type is fixed by the discriminant :
| Condition | Type | Physical example |
|---|---|---|
| Elliptic | Laplace/Poisson equation — steady-state heat / potential / electrostatics | |
| Parabolic | Heat (diffusion) equation — transient heat conduction | |
| Hyperbolic | Wave equation — vibrating string / wave propagation |
Worked check: For Laplace, (elliptic). For the heat equation written in two variables, the second-order part has (parabolic). For the wave equation , (hyperbolic).
Section B: Short Answer Questions
Attempt all / any as specified.
Find a real root of the equation correct to four significant figures using the Secant method. Take the initial approximations and and tabulate the successive iterations.
Secant Method for
Write . The secant iteration is
With :
| n | ||||
|---|---|---|---|---|
| 1 | 0.50000 | 0.60000 | 0.607193 | |
| 2 | 0.60000 | 0.607193 | 0.607102 | |
| 3 | 0.607193 | 0.607102 | 0.607102 |
Sample step (n=1):
The successive iterates agree to four significant figures, so
Evaluate the integral by dividing the interval into six equal subintervals using (a) the Trapezoidal rule and (b) Simpson's 1/3 rule. Compare your results with the exact value.
Numerical Integration of
With 6 subintervals, . Tabulate :
| 0 | 1 | 2 | 3 | 4 | 5 | 6 | |
|---|---|---|---|---|---|---|---|
| 1.0000 | 0.5000 | 0.2000 | 0.1000 | 0.058824 | 0.038462 | 0.027027 |
(a) Trapezoidal Rule
(b) Simpson's 1/3 Rule
Comparison with exact value
| Method | Result | Error |
|---|---|---|
| Trapezoidal | 1.4108 | |
| Simpson 1/3 | 1.3662 | |
| Exact | 1.40565 | — |
The trapezoidal value is closer here because the integrand changes rapidly near ; Simpson's rule, though normally more accurate, is more affected by the coarse mesh over this steep region.
From the following table of values, find the first and second derivatives of at using Newton's forward difference formula:
| x | 1.0 | 1.2 | 1.4 | 1.6 | 1.8 | 2.0 |
|---|---|---|---|---|---|---|
| f(x) | 0.000 | 0.128 | 0.544 | 1.296 | 2.432 | 4.000 |
Numerical Differentiation by Newton's Forward Formula
Here , . The forward difference table:
| 1.0 | 0.000 | 0.128 | 0.288 | 0.048 |
| 1.2 | 0.128 | 0.416 | 0.336 | 0.048 |
| 1.4 | 0.544 | 0.752 | 0.384 | 0.048 |
| 1.6 | 1.296 | 1.136 | 0.432 | |
| 1.8 | 2.432 | 1.568 | ||
| 2.0 | 4.000 |
Third differences are constant () and higher differences vanish.
For : .
First derivative
With : , .
Second derivative
Thus at , and .
Fit a straight line to the following data using the method of least squares and estimate the value of when :
| x | 1 | 2 | 3 | 4 | 5 |
|---|---|---|---|---|---|
| y | 1.2 | 1.8 | 3.3 | 4.5 | 6.3 |
Least-Squares Straight Line
Normal equations:
| 1 | 1.2 | 1 | 1.2 |
| 2 | 1.8 | 4 | 3.6 |
| 3 | 3.3 | 9 | 9.9 |
| 4 | 4.5 | 16 | 18.0 |
| 5 | 6.3 | 25 | 31.5 |
| 17.1 | 55 | 64.2 |
with . The normal equations:
Solving (e.g. ):
Fitted line:
Estimate at :
Using the fourth-order Runge-Kutta method, find an approximate value of at for the initial value problem , , taking a step size .
Fourth-Order Runge-Kutta Method
Given , , . RK4:
Step 1:
Step 2:
Using the LU (Doolittle) decomposition method, factorize the coefficient matrix and solve the system:
LU (Doolittle) Decomposition
In Doolittle's method with unit diagonal in :
Row 1 of U: Column 1 of L: Row 2 of U: : :
Forward substitution :
Back substitution :
(equivalently ).
Using the explicit (Bender-Schmidt) finite-difference scheme, solve the one-dimensional heat conduction equation subject to , for . Take and choose an appropriate time step satisfying the stability criterion; compute for the first two time levels.
Bender-Schmidt Explicit Scheme for the Heat Equation
The explicit finite-difference form of is
where , . Stability requires . Choosing the Bender-Schmidt value gives the simplified average formula
With , Mesh nodes .
Initial values , with boundaries for all :
Level ():
Level ():
| 0.25 | 0.50 | 0.75 | |||
|---|---|---|---|---|---|
| 0.00000 | 0 | 0.7071 | 1.0000 | 0.7071 | 0 |
| 0.03125 | 0 | 0.5000 | 0.7071 | 0.5000 | 0 |
| 0.06250 | 0 | 0.3536 | 0.5000 | 0.3536 | 0 |
The solution decays symmetrically, consistent with the exact solution .
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